-
1.发明申请SYSTEM AND METHOD FOR PREDICTION OF GAS TURBINE TRIPS DUE TO THERMOCOUPLE FAILURES 有权用于预测热电偶故障的气体涡轮机的系统和方法公开(公告)号：US20090055070A1
公开(公告)日：2009-02-26
申请号：US11843939
申请日：2007-08-23
申请人： Soumen De , Ravi Yoganatha Babu , Vinay Bhaskar Jammu , Achalesh Kumar Pandey , Richard John Rucigay
发明人： Soumen De , Ravi Yoganatha Babu , Vinay Bhaskar Jammu , Achalesh Kumar Pandey , Richard John Rucigay
IPC分类号： F02D28/00
CPC分类号： F02C9/00 , F05D2260/80 , G05B23/0283
摘要： Systems and methods for prediction of gas turbine trips due to component failures such as thermocouple failures. Exemplary embodiments include prediction of gas turbine trips due to component failures, including collecting raw gas turbine operational data and using the raw gas turbine operational data to generate a prognostic indicator for the prediction of a turbine trip due to the failed thermocouples.
摘要翻译： 由于组件故障（如热电偶故障）预测燃气轮机跳闸的系统和方法。 示例性实施例包括由于部件故障而预测燃气轮机跳闸，包括收集原始燃气轮机操作数据并使用原燃气涡轮机操作数据来产生预测由于故障热电偶引起的涡轮机跳闸的预测指示器。
-
公开(公告)号：US20110211940A1
公开(公告)日：2011-09-01
申请号：US12714207
申请日：2010-02-26
申请人： Sheri George , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Chayan Mitra , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Bhasker Rao Keely , Munish Vishwas Inamdar
发明人： Sheri George , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Chayan Mitra , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Bhasker Rao Keely , Munish Vishwas Inamdar
CPC分类号： F01D21/003 , F01D25/285 , F05D2260/80 , F05D2270/8041 , G01N21/954 , G01N2021/8887 , Y02T50/671
摘要： Embodiments of the invention include an inspection system to inspect internal components of a compressor of a gas turbine engine. The inspection system includes an image recording assembly having one or more image recording devices, light sources, storage devices, and power supplies. The image recording assembly may be inserted into a compressor without removal of the compressor housing or disassembly of the compressor. The image recording assembly may be removably coupled to a rotary component of the compressor, e.g., a rotor blade, and used to record images of stationary components, e.g., stator vanes, of the compressor. The images may be inspected to identify wear and/or defects in the stationary components, e.g., stator vanes
摘要翻译： 本发明的实施例包括检查燃气涡轮发动机的压缩机的内部部件的检查系统。 检查系统包括具有一个或多个图像记录装置，光源，存储装置和电源的图像记录组件。 图像记录组件可以插入压缩机中，而不需要拆除压缩机壳体或压缩机的拆卸。 图像记录组件可以可拆卸地联接到压缩机的旋转部件，例如转子叶片，并用于记录压缩机的静止部件（例如定子叶片）的图像。 可以检查图像以识别固定部件（例如定子叶片）中的磨损和/或缺陷
-
3.发明授权Image recording assemblies and coupling mechanisms for stator vane inspection 有权用于定子叶片检查的图像记录组件和联接机构公开(公告)号：US08587660B2
公开(公告)日：2013-11-19
申请号：US12847909
申请日：2010-07-30
申请人： Chayan Mitra , Munish Vishwas Inamdar , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Sheri George , Bhasker Rao Keely
发明人： Chayan Mitra , Munish Vishwas Inamdar , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Sheri George , Bhasker Rao Keely
IPC分类号： H04N7/18
CPC分类号： H04N7/18 , G01N29/0654
摘要： A system is disclosed that includes an image recording assembly for recording images of a stator vane of a compressor and a mechanism configured to magnetically couple the image recording assembly to a rotor blade of a compressor. Additional systems are provided that include image recording assemblies. Methods implementing the disclosed systems are also provided.
摘要翻译： 公开了一种系统，其包括用于记录压缩机的定子叶片的图像的图像记录组件和被配置为将图像记录组件磁耦合到压缩机的转子叶片的机构。 提供了包括图像记录组件的附加系统。 还提供了实现所公开的系统的方法。
-
公开(公告)号：US09122991B2
公开(公告)日：2015-09-01
申请号：US13600387
申请日：2012-08-31
CPC分类号： G06N5/04 , F01D21/00 , F02C9/00 , F05D2260/80 , F05D2270/44 , G05B23/0283
摘要： A system is disclosed. The system includes a processing subsystem that receives component data signals corresponding to a plurality of parameters of a device, wherein the processing subsystem generates one or more sets of state category component data by allocating the component data signals into respective one or more sets of state category component data, determines a plurality of first dynamic thresholds and a plurality of second dynamic thresholds corresponding to at least one of the one or more sets of state category component data based upon a respective set of state category component data in the one or more sets of state category component data and a respective parameter in the plurality of parameters, and determines an impending trip of the device utilizing the plurality of first dynamic thresholds and the plurality of second dynamic thresholds.
摘要翻译： 公开了一种系统。 该系统包括处理子系统，其接收对应于设备的多个参数的分量数据信号，其中处理子系统通过将分量数据信号分配到相应的一组或多组状态类别中来生成一组或多组状态类别分量数据 组件数据，基于一组或多组状态类别组件数据中的相应集合，确定与所述一组或多组状态类别分量数据中的至少一个对应的多个第一动态阈值和多个第二动态阈值 状态类别分量数据和多个参数中的相应参数，并且使用多个第一动态阈值和多个第二动态阈值来确定设备的即将跳闸。
-
公开(公告)号：US08471702B2
公开(公告)日：2013-06-25
申请号：US12976255
申请日：2010-12-22
CPC分类号： F04B51/00 , F02C9/00 , F05D2260/80 , G01M15/14
摘要： A method for monitoring the health of a compressor of a gas turbine is disclosed. The method includes receiving a plurality of turbine data points, wherein the plurality of turbine data points may include one or more operating parameters, at least one of a computer discharge temperature (CTD), and one or more performance parameters. The plurality of turbine data points may be categorized based on the one or more operating parameters. A statistical variability measure of at least one of the CTD and the one or more performance parameters may be computed for each of the plurality of bands. An alarm indicator may be computed based on the at least one statistical variability measure. The method may also include combining two or more of the operating parameters, the CTD and the performance parameters using sensor fusion techniques. The alarm indicator may be computed based on the combined parameters.
摘要翻译： 公开了一种用于监测燃气轮机的压缩机的健康状况的方法。 该方法包括接收多个涡轮数据点，其中多个涡轮数据点可以包括一个或多个运行参数，计算机排放温度（CTD）和一个或多个性能参数中的至少一个。 可以基于一个或多个操作参数对多个涡轮数据点进行分类。 可以为多个频带中的每个频带计算CTD和一个或多个性能参数中的至少一个的统计变异性度量。 可以基于至少一个统计变异性度量来计算报警指示符。 该方法还可以包括使用传感器融合技术组合两个或多个操作参数，CTD和性能参数。 可以基于组合的参数来计算报警指示符。
-
6.发明申请SYSTEM AND METHOD FOR PREDICTION OF GAS TURBINE TRIPS DUE TO GAS CONTROL VALVE FAILURES 有权用于气体控制阀故障预测气体涡轮机的系统和方法公开(公告)号：US20090055130A1
公开(公告)日：2009-02-26
申请号：US11843951
申请日：2007-08-23
IPC分类号： G06F11/30
CPC分类号： G05B23/0254
摘要： Systems and methods for prediction of gas turbine trips due to component failures such as electro-hydraulic valve (gas control valve) system failures. Exemplary embodiments include prediction of gas turbine trips due to component failures, the method including collecting raw gas turbine operational data and using the raw gas turbine operational data to generate a prognostic indicator for the prediction of a turbine trip due to the failed gas control valves.
摘要翻译： 用于预测由电液阀（气体控制阀）系统故障引起的部件故障引起的燃气轮机跳闸的系统和方法。 示例性实施例包括由于部件故障而导致的燃气轮机跳闸的预测，该方法包括收集原燃气涡轮机操作数据并使用原始燃气涡轮机操作数据来生成用于预测由于气体控制阀故障引起的涡轮机跳闸的预测指示器。
-
公开(公告)号：US08602722B2
公开(公告)日：2013-12-10
申请号：US12714207
申请日：2010-02-26
申请人： Sheri George , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Chayan Mitra , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Bhasker Rao Keely , Munish Vishwas Inamdar
发明人： Sheri George , Vinay Bhaskar Jammu , Vinod Padmanabhan Kumar , Chayan Mitra , Kunal Ravindra Goray , Achalesh Kumar Pandey , Ravi Yoganatha Babu , Bhasker Rao Keely , Munish Vishwas Inamdar
IPC分类号： F01D25/00
CPC分类号： F01D21/003 , F01D25/285 , F05D2260/80 , F05D2270/8041 , G01N21/954 , G01N2021/8887 , Y02T50/671
摘要： Embodiments of the invention include an inspection system to inspect internal components of a compressor of a gas turbine engine. The inspection system includes an image recording assembly having one or more image recording devices, light sources, storage devices, and power supplies. The image recording assembly may be inserted into a compressor without removal of the compressor housing or disassembly of the compressor. The image recording assembly may be removably coupled to a rotary component of the compressor, e.g., a rotor blade, and used to record images of stationary components, e.g., stator vanes, of the compressor. The images may be inspected to identify wear and/or defects in the stationary components, e.g., stator vanes.
摘要翻译： 本发明的实施例包括检查燃气涡轮发动机的压缩机的内部部件的检查系统。 检查系统包括具有一个或多个图像记录装置，光源，存储装置和电源的图像记录组件。 图像记录组件可以插入压缩机中，而不需要拆除压缩机壳体或压缩机的拆卸。 图像记录组件可以可拆卸地联接到压缩机的旋转部件，例如转子叶片，并用于记录压缩机的静止部件（例如定子叶片）的图像。 可以检查图像以识别固定部件（例如定子叶片）中的磨损和/或缺陷。
-
8.发明授权System and method for prediction of gas turbine trips due to gas control valve failures 有权由于气体控制阀故障导致的燃气轮机跳闸预测的系统和方法公开(公告)号：US08250017B2
公开(公告)日：2012-08-21
申请号：US11843951
申请日：2007-08-23
CPC分类号： G05B23/0254
摘要： Systems and methods for prediction of gas turbine trips due to component failures such as electro-hydraulic valve (gas control valve) system failures. Exemplary embodiments include prediction of gas turbine trips due to component failures, the method including collecting raw gas turbine operational data and using the raw gas turbine operational data to generate a prognostic indicator for the prediction of a turbine trip due to the failed gas control valves.
摘要翻译： 用于预测由电液阀（气体控制阀）系统故障引起的部件故障引起的燃气轮机跳闸的系统和方法。 示例性实施例包括由于部件故障而导致的燃气轮机跳闸的预测，该方法包括收集原燃气涡轮机操作数据并使用原始燃气涡轮机操作数据来生成用于预测由于气体控制阀故障引起的涡轮机跳闸的预测指示器。
-
公开(公告)号：US20120161965A1
公开(公告)日：2012-06-28
申请号：US12976255
申请日：2010-12-22
IPC分类号： G08B21/00
CPC分类号： F04B51/00 , F02C9/00 , F05D2260/80 , G01M15/14
摘要： A method for monitoring the health of a compressor of a gas turbine is disclosed. The method includes receiving a plurality of turbine data points, wherein the plurality of turbine data points may include one or more operating parameters, at least one of a computer discharge temperature (CTD), and one or more performance parameters. The plurality of turbine data points may be categorized based on the one or more operating parameters. A statistical variability measure of at least one of the CTD and the one or more performance parameters may be computed for each of the plurality of bands. An alarm indicator may be computed based on the at least one statistical variability measure. The method may also include combining two or more of the operating parameters, the CTD and the performance parameters using sensor fusion techniques. The alarm indicator may be computed based on the combined parameters.
摘要翻译： 公开了一种用于监测燃气轮机的压缩机的健康状况的方法。 该方法包括接收多个涡轮数据点，其中多个涡轮数据点可以包括一个或多个运行参数，计算机排放温度（CTD）和一个或多个性能参数中的至少一个。 可以基于一个或多个操作参数对多个涡轮数据点进行分类。 可以为多个频带中的每个频带计算CTD和一个或多个性能参数中的至少一个的统计变异性度量。 可以基于至少一个统计变异性度量来计算报警指示符。 该方法还可以包括使用传感器融合技术组合两个或多个操作参数，CTD和性能参数。 可以基于组合的参数来计算报警指示符。
-
公开(公告)号：US20140244567A1
公开(公告)日：2014-08-28
申请号：US13600387
申请日：2012-08-31
IPC分类号： G06N5/04
CPC分类号： G06N5/04 , F01D21/00 , F02C9/00 , F05D2260/80 , F05D2270/44 , G05B23/0283
摘要： A system is disclosed. The system includes a processing subsystem that receives component data signals corresponding to a plurality of parameters of a device, wherein the processing subsystem generates one or more sets of state category component data by allocating the component data signals into respective one or more sets of state category component data, determines a plurality of first dynamic thresholds and a plurality of second dynamic thresholds corresponding to at least one of the one or more sets of state category component data based upon a respective set of state category component data in the one or more sets of state category component data and a respective parameter in the plurality of parameters, and determines an impending trip of the device utilizing the plurality of first dynamic thresholds and the plurality of second dynamic thresholds.
摘要翻译： 公开了一种系统。 该系统包括处理子系统，其接收对应于设备的多个参数的分量数据信号，其中处理子系统通过将分量数据信号分配到相应的一组或多组状态类别中来生成一组或多组状态类别分量数据 组件数据，基于一组或多组状态类别组件数据中的相应集合，确定与所述一组或多组状态类别分量数据中的至少一个对应的多个第一动态阈值和多个第二动态阈值 状态类别分量数据和多个参数中的相应参数，并且使用多个第一动态阈值和多个第二动态阈值来确定设备的即将跳闸。
-
-
-
-
-
-
-
-
-
搜索结果
43 条记录 (耗时 0.018 秒)
